Books on the topic 'Turbomachinery flow'

Max, Platzer, Carta Franklin O, North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel., and North Atlantic Treaty Organization. Advisory Groupfor Aerospace research and Development. Structures and Materials Panel., eds. AGARD manual on aeroelasticity in axial-flow turbomachines. Volume 1: Unsteady turbomachinery aerodynamics. AGARD, 1987.

K, Choo Yung, Eiseman Peter R, Reno Charles J, and Lewis Research Center, eds. Interactive grid generation for turbomachinery flow field simulations. National Aeronautics and Space Administration, Lewis Research Center, 1988.

Caughey, D. A. Multigrid calculation of three-dimensional turbomachinery flows. Fluid Dynamics and Aerodynamics Program, Sibley School of Mechanical and Aerospace Engineering, Cornell University, 1989.

United States. National Aeronautics and Space Administration, ed. Multigrid calculation of three-dimensional turbomachinery flows. Fluid Dynamics and Aerodynamics Program, Sibley School of Mechanical and Aerospace Engineering, Cornell University, 1989.

Center, Lewis Research, ed. Validation of viscous and inviscid computational methods for turbomachinery components. National Aeronautics and Space Administration, Lewis Research Center, 1986.

A, Mulac Richard, Celestina Mark L, and Lewis Research Center, eds. A model for closing the inviscid form of the average-passage equation system. National Aeronautics and Space Administration, Lewis Research Center, 1986.

Center, Lewis Research, and United States. Army Aviation Systems Command., eds. Computer code for predicting coolant flow and heat transfer in turbomachinery. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

United States. National Aeronautics and Space Administration., ed. Current Lewis turbomachinery research: Building on our legacy of excellence. National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration., ed. Towards a comprehensive computational simulation system for turbomachinery. National Aeronautics and Space Administration, 1994.

Center, Lewis Research, ed. A FORTRAN computer code for calculating flows in multiple-blade-element cascades. National Aeronautics and Space Administration, Lewis Research Center, 1985.

P, Van Hooser Katherine, and United States. National Aeronautics and Space Administration., eds. A general fluid system simulation program to model secondary flows in turbomachinery. National Aeronautics and Space Administration, 1995.

1913-, Hawthorne William Sir, and United States. National Aeronautics and Space Administration., eds. Three-dimensional flow in radial turbomachinery and its impact on design. Gas Turbine Laboratory, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology, 1993.

D, Montgomery Matthew, Kousen Kenneth A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Development of a linearized unsteady Euler analysis for turbomachinery blade rows. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

D, Montgomery Matthew, Kousen Kenneth A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Development of a linearized unsteady Euler analysis for turbomachinery blade rows. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

United States. National Aeronautics and Space Administration., ed. An interactive grid generation procedure for axial and radial flow turbomachinery. National Aeronautics and Space Administration, 1990.

Center, Lewis Research, ed. PSP measurement of stator vane surface pressures in a high speed fan. National Aeronautics and Space Administration, Lewis Research Center, 1998.

M, Verdon Joseph, and United States. National Aeronautics and Space Administration., eds. A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows. National Aeronautics and Space Administration, 1996.

J, Roelke Richard, Meitner Peter L, and United States. National Aeronautics and Space Administration., eds. A generalized one dimensional computer code for turbomachinery cooling passage flow calculations. National Aeronautics and Space Administration, 1989.

O, Carta F., and North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development., eds. AGARD manual on aeroelasticity in axial-flow turbomachines, vol.2. Structural dynamics and aeroelasticity. AGARD, 1988.

M, Verdon Joseph, and United States. National Aeronautics and Space Administration., eds. A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows. National Aeronautics and Space Administration, 1996.

Montgomery, Matthew D. A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

United States. National Aeronautics and Space Administration., ed. Solutions to three-dimensional thin-layer Navier-Stokes equations in rotating coordinates for flow through turbomachinery. National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., ed. Solutions to three-dimensional thin-layer Navier-Stokes equations in rotating coordinates for flow through turbomachinery. National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., ed. Solutions to three-dimensional thin-layer Navier-Stokes equations in rotating coordinates for flow through turbomachinery. National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., ed. Solutions to three-dimensional thin-layer Navier-Stokes equations in rotating coordinates for flow through turbomachinery. National Aeronautics and Space Administration, 1996.

Lepicovsky, Jan. Use of pressure sensitive paint for diagnostics in turbomachinery flows with shocks. National Aeronautics and Space Administration, Glenn Research Center, 2000.

C, Hall Kenneth, and United States. National Aeronautics and Space Administration., eds. Sensitivity analysis for aeroacoustic and aeroelastic design of turbomachinery blades: Final technical report. Dept. of Mechanical Engineering and Materials Science, School of Engineering, Duke University, 1995.

United States. National Aeronautics and Space Administration., ed. Calculation of three-dimensional, viscous flow through turbomachinery blade passages by parabolic marching. National Aeronautics and Space Administration, 1985.

United States. National Aeronautics and Space Administration., ed. Calculation of three-dimensional, viscous flow through turbomachinery blade passages by parabolic marching. National Aeronautics and Space Administration, 1985.

United States. National Aeronautics and Space Administration., ed. Calculation of three-dimensional, viscous flow through turbomachinery blade passages by parabolic marching. National Aeronautics and Space Administration, 1985.

United States. National Aeronautics and Space Administration., ed. Calculation of three-dimensional, viscous flow through turbomachinery blade passages by parabolic marching. National Aeronautics and Space Administration, 1985.

Chung-hua, Wu. A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Chung-hua, Wu. A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

M, Sindir Munir, and United States. National Aeronautics and Space Administration., eds. Comparative study of advanced turbulence models for turbomachinery: Contract NAS8-38860, final report. National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., ed. Unsteady blade row interaction in a transonic turbine: Final report, NASA grant NAG3-1671. National Aeronautics and Space Administration, 1996.

S, Clark William. Prediction of unsteady flows in turbomachinery using the linearized Euler equations on deforming grids. National Aeronautics and Space Administration, 1991.

S, Clark William. Prediction of unsteady flows in turbomachinery using the linearized Euler equations on deforming grids. National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Steinke, Ronald J. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Steinke, Ronald J. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. Lewis Research Center, 1989.

M, Verdon Joseph, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows: Under contract NAS3-26618. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

1945-, Sharma Om P., and United States. National Aeronautics and Space Administration., eds. Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines. National Aeronautics and Space Administration, 1997.

A, Myers R., Delaney Robert A, and United States. National Aeronautics and Space Administration., eds. TADS, a CFD-based turbomachinery and analysis design system with GUI. National Aeronautics and Space Administration, 1995.